Heat exchanger having powder coated elements

ABSTRACT

Powder coated heat exchange elements for a heat exchanger. Powder coating provides improved protective coating on surfaces of heat exchange elements. In many applications, the heat exchange elements are subjected to harsh operating conditions that promote corrosion. Traditional enamel coating tends to fracture when subjected to mechanical stresses thereby allowing corrosion inducing agents to penetrate and corrode the underlying surfaces. Powder coating reduces breaches in the protective layer. Powder coating may be adapted to withstand high temperatures so as to make them suitable for use in harsh operating environments. One such environment can be found in the processing of flue gas from fossil burning power generators, where the flue gas has a relatively high temperature and high sulfur content.

RELATED APPLICATIONS

This application is a continuation application of U.S. patent Ser. No.12/911,346 filed on Oct. 25, 2010, which is a continuation applicationof U.S. patent application Ser. No. 11/198,406, filed Aug. 4, 2005, nowU.S. Pat. No. 7,819,176, which is a continuation-in-part application ofU.S. application Ser. No. 10/793,182, filed Mar. 3, 2004, now U.S. Pat.No. 7,841,390, which claims the benefit of U.S. Provisional ApplicationNo. 60/452,065, filed Mar. 3, 2003 and entitled “ROTARY HEAT EXCHANGERWITH POWDER COATED HEAT EXCHANGE ELEMENTS”, all of which are herebyincorporated by reference in their entirety and should be considered apart of this specification.

BACKGROUND

1. Field

The present teachings relate to heat exchangers and, in particular,relates to a heat exchanger having powder coated elements that inhibitcorrosion.

2. Description of the Related Art

Heat exchangers in various forms are included in systems that controlthe condition of air. Conventional heat exchangers include a heater thattakes input air and outputs air with a higher temperature. A cooler,generally referred to as an air conditioner, takes input air and outputsair with a lower temperature. In both cases, the change in temperatureis achieved by some form of a heat exchanger. In a heater, air istypically blown past a heated element such that heat is transferred fromthe heated element to the air. In a cooler, air is typically blown pasta chilled element such that heat is transferred from the air to thechilled element.

A rotary heat exchanger is an apparatus that exchanges heat withrelatively large volumes of air. The rotary heat exchanger typicallycomprises a cylindrically shaped device that permits air to flowtherethrough. Typically, heat exchange is achieved by flowing both theinput air and exhaust air through the rotating rotary heat exchanger attwo different locations. Heat exchange elements in the exchanger removeheat from one flow of air and release the heat to the other flow of air.The rotational speed can be selected to permit efficient overall heattransfer.

In operation, the heat exchangers are usually exposed to harshenvironments that tend to induce corrosion of the metal of the heatexchanger, including the seals and the heat exchange elements. Thecorrosive environment leads to pitting in the degeneration of the metalin the heat exchange elements, structurally weakening the elements. Tocounter the corrosion problems, traditional heat exchange elements oftenhave an enamel coating applied to the surface of the metal. Often, theenamel coating contains bubbles such that full corrosion protection isnot afforded. In addition, the enamel coating is susceptible to crackingwhen subjected to mechanical stresses. Such breach of the coating allowscorrosion inducing agents to come in contact with the metal, therebycausing corrosion, which in turn reduces the effectiveness of the heatexchanger.

From the foregoing, it will be appreciated that there is a need for animproved method of fabricating a heat exchanger. To this end, there alsoexists a need for an improved method of protecting the metal of the heatexchange elements so as to provide improved corrosion resistance.

SUMMARY

The aforementioned needs may be satisfied by a heat exchangercomprising, in one embodiment, a heat exchanging body that rotates in afirst direction with respect to a housing and a plurality of heatexchange elements disposed in the heat exchanging body so as to define aplurality of channels that allow air to flow therethrough, wherein eachheat exchange element includes a powder coating to thereby resistcorrosion.

In one aspect, the heat exchanging body comprises a rotor. The rotor maybe adapted to rotate about a rotational axis with respect to the housingsuch that a given portion of the rotor gains heat energy at a firstlocation and gives off heat energy at a second location. In addition,the heat exchanger further comprises a first air passage assemblydisposed adjacent the heat exchanging body, and wherein the air passageassembly is adapted to allow air to flow through a portion of the heatexchange body. Also, the first air passage assembly is disposed adjacentthe rotor at one of the first or second locations. The air passageassembly is adapted to allow flow of air through a portion of the heatexchange body along a first direction relative to the rotational axis.The first direction is substantially parallel to the rotational axis.Moreover, the heat exchanging body is divided into a plurality ofsectors, and wherein each sector includes at least one heat exchangeelement positioned therein.

In another aspect, the powder coating comprises a high silica content.The powder coating is applied to the heat exchange elements with atemperature cure of approximately 400-500° F., 400-450° F. in about 15minutes, or 400° F. in about 60 minutes. Also, the powder coating isadapted to withstand approximately 1000° F. for approximately 24 hours.The thickness of the powder coating on the heat exchange elements isbetween approximately 1.5-2.5 mils, or the thickness is betweenapproximately 2-4 mils. Moreover, the powder coating comprises a layerof fused powder applied to the heat exchange elements in anelectrostatically charged powder form and cured by heat.

In still another aspect, the heat exchanger is adapted to be used in ahigh sulfur content air and high temperature environment. Also, the heatexchanger is adapted to be used to reduce the temperature of a flue gasbeing emitted from a fossil burning power generator prior to the gasbeing ejected into the environment.

The aforementioned needs may also be satisfied with a heat exchangercomprising, in one embodiment, a heat exchanging body that rotates withrespect to a housing and a first air passage assembly disposed adjacentthe heat exchanging body, wherein the air passage assembly is adapted toallow flow of air through a portion of the heat exchange body. Inaddition, the heat exchanger may further comprise a plurality of heatexchange elements disposed in the heat exchanging body, wherein eachheat exchange element defines a heat exchanging surface adapted tofacilitate the heat exchange with the air flowing through the heatexchanging body, and wherein the heat exchanging surface includes apowder coating that resists corrosion.

In one aspect, the heat exchanging body defines a plurality of segments,and wherein each segment defines a volume dimensioned to receive aplurality of heat exchange elements, and wherein each segment extendsfrom a first angle to a second angle so as to generally resemble apie-slice shape when viewed along the rotational axis. In addition, theheat exchange elements comprise shaped sheets of material dimensioned soas to be stackable along a radial direction, and wherein the shapedsheets are oriented so as to allow flow of air with a net direction thatis generally parallel to the rotational axis. Also, the shaped sheetscomprise a material selected from the group consisting of a sheet ofmetal, a sheet of stainless steel, a sheet of low carbon steel. Thethickness of the shaped sheet is between approximately 18-24 gauge.Moreover, the shaped sheets define a plurality of channels for the flowof air such that, when stacked, the channels extend in a directionsubstantially parallel to the rotational axis. The shaped sheetscomprises a first type of sheet and a second type of sheet such that thefirst type of sheet defines a plurality of channels that extend along afirst direction relative to the rotational axis and the second type ofsheet defines a plurality of channels that extend along a seconddirection relative to the rotational axis. The channels of the firsttype of sheet and the channels of the second type of sheet form crossingpatterns.

The aforementioned needs may also be satisfied by a heat exchangeassembly for a heat exchanger having a heat exchanging body that rotatesin a first direction with respect to a housing. In one embodiment, theassembly comprises a plurality of heat exchange members that are formedso as define a heat exchange surface, wherein the heat exchange membersare positioned in the heat exchanging body to thereby facilitate heatexchange with air. In addition, the assembly further comprises aprotective layer disposed on the heat exchange surface, wherein theprotective layer comprises a powder coating that inhibits corrosion ofthe heat exchange members.

In one aspect, the heat exchange members comprise a cross sectionalshape including a plurality or undulations separated by a flat section,and wherein each undulated shape comprises an upper curved shape joinedto a lower curved shape so as to form a full cycle wave like structure.In addition, the heat exchange members may comprise a corrugatedconfiguration or a notched flat configuration. Moreover, the powdercoating provides a barrier for the underlying heat exchange members tothereby resist corrosion inducing agents including water and sulfurbased compounds.

The aforementioned needs may also be satisfied by a method offabricating a heat exchanger having a plurality of heat exchangeelements adapted to allow flow of air therethrough and exchange heatwith the flowing air. In one embodiment, the method comprises preparingthe heat exchange elements for assembly, powder coating the heatexchange elements, and assembling the heat exchange elements. In oneaspect, powder coating the heat exchange elements comprises cleaning thesurface of the heat exchange elements and electrically grounding theheat exchange elements. In addition, powder coating the heat exchangeelements further comprises applying electrostatically charged coatingparticles onto the heat exchange elements wherein the electrostaticallycharged coating particles are attracted to the electrically ground heatexchange elements thereby promoting adhesion of the coating particles tothe surfaces of the heat exchange elements and curing the heat exchangeelements, e.g. via the application of heat, so as to cause the coatingparticles to fuse with the surfaces of the heat exchange elements.

The aforementioned needs may also be satisfied by a method of applying acorrosion resistant coating on a heat exchange element adapted for usein a heat exchanger. In one embodiment, the method comprises preparingthe surface of the heat exchange element and electrically connecting theheat exchange element to a first potential. In addition, the methodcomprises applying electrostatically charged coating particles onto theheat exchange element wherein the first potential and the electrostaticcharge of the coating particles are selected to promote adhesion of thecoating particles to the surface of the heat exchange element and curingthe heat exchange element so as to cause the coating particles to fusewith the surface of the heat exchange element. In one aspect, preparingthe surface comprises cleaning the surface so as to facilitate adhesionof the coating particles. In addition, electrically connecting the heatexchange element comprises electrically grounding the heat exchangeelement.

These and other advantages of the present teachings will become morefully apparent from the following description taken in conjunction withthe accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1A illustrates a side view of an exemplary rotary heat exchanger.

FIG. 1B illustrates an end view of an exemplary rotary heat exchanger.

FIG. 2 illustrates a segment of a rotor of the rotary heat exchanger,wherein the segment comprises a plurality of heat exchange elementsstacked within a defined volume.

FIGS. 3A-3E illustrate some of the various possible configurations ofthe heat exchange elements.

FIGS. 4A-4B illustrate powder coated surfaces of the heat exchangeelement.

FIG. 5 illustrates one possible method of fabricating a heat exchangerhaving powder coated heat exchange elements.

FIG. 6 illustrates one possible method of powder coating a heat exchangeelement.

FIG. 7 illustrates one possible application of the heat exchanger havingpowder coated heat exchange elements, wherein the powder coating may beadapted to operate at high temperatures.

FIG. 8 illustrates another embodiment of a method of powder coating acomponent of a heat exchanger.

FIG. 9 is a perspective view of one embodiment of a seal assembly.

FIG. 10 is a side view of the seal assembly of FIG. 9 in one operatingposition.

FIG. 11A is a partial cross-sectional view of a heat exchangerillustrating another embodiment of a seal assembly.

FIG. 11B is a partial cross-sectional view of a heat exchangerillustrating the seal assembly of FIG. 11A mounted in differentconfiguration in the heat exchanger.

FIG. 12 is a perspective assembled view of the seal assembly of FIG.11A.

FIG. 13 is a top view of the seal assembly of FIG. 12.

DETAILED DESCRIPTION

In the following detailed description, terms of orientation such as“top,” “bottom,” “upper,” “lower,” “front,” “rear,” and “end” are usedherein to simplify the description of the context of the illustratedembodiments. Likewise, terms of sequence, such as “first” and “second,”are used to simplify the description of the illustrated embodiments.Because other orientations and sequences are possible, however, thepresent invention should not be limited to the illustrated orientation.Those skilled in the art will appreciate that other orientations of thevarious components described below are possible.

Reference will now be made to the drawings wherein like numerals referto like parts throughout. FIGS. 1A-7 illustrate various aspects relatedto a heat exchanger having powder coated elements that inhibitcorrosion. Various other aspects of the present teachings will bedescribed in greater detail herein below with reference to the drawings.In general, it should be appreciated that the following description of aheat exchanger and elements comprised therein is in the context of arotary heat exchanger. However, it should be appreciated by thoseskilled in the art that the novel features described herein are notlimited to rotary type devices, but may be applied to various othertypes of generally known heat exchangers.

FIG. 1A illustrates a perspective view of a regenerative heat exchanger100 having one or more powder coated elements that inhibit corrosion.FIG. 1B illustrates a top view of the heat exchanger 100. As illustratedin FIGS. 1A-1B, the heat exchanger 100 comprises a heat exchanger bodyor rotor 102 that is positioned within a heat exchanger housing 104. Inone embodiment, the heat exchanger 100 comprises a rotary heatexchanger, wherein the heat exchanger body 102 comprises a cylindricalrotor and the heat exchanger housing 104 comprises a cylindricalhousing. Additionally, as further illustrated in FIGS. 1A-1B, thecylindrical rotor 102 is rotatably mounted within the cylindricalhousing 104 via a center shaft 105 so as to be coaxial therewith. Also,the heat exchanger rotor 102 further comprises a plurality of radialwalls 107 that extend radially outward from the center shaft 105.

In one embodiment, the heat exchanger housing 104 comprises first andsecond sector plates 110 a, 110 b that are respectively mounted to thefirst and second ends of the housing 104. The heat exchanger housing 104is formed so as to define at least two conduit openings 106, 108 thatform a portion of the intake or cold air conduit and the exhaust or hotgas conduit. Also, the sector plates 110 a, 110 b divide the intakeconduit from the exhaust conduit and can be connected to duct work (notshown) in a generally known manner.

In one embodiment, the plurality of radial walls 107 divides the heatexchanger rotor 102 into a plurality of sectors 112 comprising corematerial 114. The core material 114 is adapted to absorb heat carried inthe exhaust gas from the exhaust conduit and then transfer the absorbedheat to the intake air when the heated sector 112 is positioned in thepath of the intake conduit. In one aspect, the core material 114 maycomprise thin corrugated conductive material, such as metal, that allowsexhaust gases to travel therethrough. Also, heat carried within theexhaust gases heats the core material 114 in the exhaust conduit.

Similarly, cool air passing through the core material 114 in the intakeconduit is heated by the retained heat of the core material 114 duringpassage of the intake air through the core material 114. The heatexchanger 100 sequentially exposes each sector 112 to hot gas in theexhaust conduit so that the core material 114 is heated and, duringrotation, exposes the heated sectors 112 of core material 114 to theintake conduit so that cooler air traveling through the intake conduitis heated by the core material 114. The heated air is then exhaustedfrom the heat exchanger 100.

It should be appreciated that the above described heat exchanger 100 mayoperate in a similar manner to the operation of generally knownLjunstrom-type preheaters. It should also be appreciated from thefollowing description that, while this particular embodiment of theperimeter seal assembly may be configured to be used with aLjungstrom-type preheater, the perimeter seal assembly may be adapted byone skilled in the art to be used with a Rothmule-type preheater, wherethe rotor is stationary and the ductwork rotates with respect to therotor, without departing from the scope of the present teachings.

FIG. 2 illustrates one embodiment of the core material 114 formed in theplurality of sectors 112 of the heat exchanger rotor 102. As illustratedin FIG. 2, the core material 114 may comprise a wedge shaped enclosureformed by a top plate 131, a bottom plate 132, and at least two sideplates 133. The plates 131, 132, 133 may be adapted to define a cavitywithin which a plurality of heat exchange elements 140 are disposed. Inone aspect, the heat exchange elements 140 define channels 142 that arestacked adjacently together so as to permit flow of air through thechannels 142. Additionally, the channels 142 extend in a directionsubstantially parallel to the axis of rotation of the heat exchangerotor 102. Hence, the air flow 148 can be in a direction relative to theaxis of rotation.

In the embodiment, the heat exchange elements 140 are formed withcorrugated and flat material, such as corrugated and flat sheet metal,that are joined together in a manner so as to form triangular shapedchannels 142. In addition, as illustrated in FIG. 2, the channels 142are layered, stacked, or arranged within the segment 130 so as to fillthe sector 112 of the heat exchange rotor 102. Advantageously, thearrangement of the layered elements 140 allow increased surface areabetween the flowing air and the surface of the channels 142.

Moreover, one aspect of the present teachings relates to the heatexchange elements 140 having a resilient surface 144 that inhibitscorrosion during harsh operating conditions and environments. Forexample, in one embodiment, the resilient surface 144 of the heatexchange elements 140 comprises a powder coating applied thereto so asto define a power coated surface. Advantageously, the coated heatexchange elements 140 provide an improved resilience and reliability tothereby increase corrosion resistance more so than a typical traditionalenamel coating.

In one embodiment, the powder coating of the resilient surface 144comprises a high silica content. Examples of the powder coating materialis manufactured by TCI Powder Coatings located in Ellaville, Ga. andAlesta Powder Coatings located in Houston, Tex. In addition, the powdercoating of the resilient surface 144 is formed with a low temperaturecure of approximately 400-500° F. Under some circumstances, the curingprocess is achieved with a temperature of approximately 400-450° F. inabout 15 minutes. In other circumstances, the curing process is achievedwith a temperature of approximately 400° F. in about 60 minutes, such aswith metal materials. Advantageously, the power coating of the resilientsurface 144 of the heat exchange elements 140 is suitable for the harshoperating conditions of the heat exchanger 100. For example, in oneaspect, the powder coating material can withstand 1000° F. forapproximately 24 hours. Additionally, in one embodiment, the filmthickness of the powder coating on the heat exchange elements 140 isbetween approximately 1.5-2.5 mils. In various other embodiments, thefilm thickness of the powder coating on the heat exchange elements 140is between approximately 2-4 mils.

Conversely, conventional enameling of the resilient surface 144, as inthe prior art processes, requires an extremely high curing temperatureof at least 1500° F. Unfortunately, this extremely high temperature canwarp or deform the heat exchange elements 140, which can adverselyimpact the efficiency and reliability of the heat exchanger 100.

Furthermore, this extremely high curing temperature of the prior art canoxidize and corrode the surface of the heat exchange elements 140. Also,in some circumstances, enamel is brittle and can fracture under theharsh operating conditions and stresses of the heat exchanger 100. Forexample, in general, coal exhaust can contain sulfur compounds. If theheat exchanger is used with coal exhaust, sulfur can combine withcondensation so as to produce sulfuric acid. As a result, the sulfuricacid can corrode metal surfaces that are exposed when the enamel surfacefractures or chips off. Sometimes, a low carbon steel can be used todeter corrosion. Unfortunately, the use of low carbon steel is moreexpensive and, thus, is not necessarily economically feasible for use inheat exchangers 100. However, the present teachings of powder coatingthe heat exchange elements 140 in a manner as described herein overcomesthe deficiencies of the prior art.

It should be appreciated by those skilled in the art that the heatexchange elements 140 may comprise various other geometrical shapes,such as circular, rectangular, pentagonal, hexagonal, etc., withoutdeparting from the scope of the present teachings. Therefore, it shouldbe appreciated that the powder coating surface may be applied to heatexchange elements 140 having various cross-sectional shapes other thanthat illustrated in FIG. 2 without departing from the scope of thepresent teachings. Various configurations of heat exchange elements 140and the manner in which they can be powder coated will be described ingreater detail herein below.

FIGS. 3A-3E illustrate various embodiments of the heat exchange elements140. It should be appreciated by those skilled in the art that thefollowing embodiments of the heat exchange elements 140 compriseexemplary contours and configurations and are not meant to limit thescope of the present teachings.

FIG. 3A illustrate one embodiment of the heat exchange elements 140described above in reference to FIG. 2. As illustrated in FIG. 3A, theelements 140 may comprise a section 150 having at least one corrugatedlayer 164 disposed adjacent to at least one flat layer 162. In oneaspect, this illustrated contour or configuration of the elements 140 isformed so as to define a plurality of triangular shaped channels 142through which air flows to thereby exchange heat with the elements 140.It should be appreciated that the combination of the corrugated layer164 and the flat layer 162 may be repeated above and/or below thecombination. For example, subsequent layering of additional sections 152above and below the first section 140 can be used to form the corematerial 114 and at least partially fill the plurality of sectors 112 ofthe heat exchange rotor 102 as illustrated in FIGS. 1A-1B.

FIG. 3B illustrates another embodiment 170 of the heat exchange elements140 comprising an undulation layer 176 disposed on a flat layer 174. Asillustrated in FIG. 3B, the sectional shape of the undulation layer 176comprises a series of undulations 180 spaced at selected distancesapart. In addition, each undulation 180 comprises an upper curved shape184 joined to a lower curved shape 186 so as to define at least onecycle resembling a wave-like structure. Also, as further illustrated inFIG. 3B, two neighboring undulation sections 180 are separated by atleast one flat section 188, wherein the undulation section 180 and theflat section 188 define a plurality of channels 182 through which aircan flow. In one aspect, it should be appreciated that the combinationof undulation and flat sections 180, 188 may be sequentially repeated.Alternatively, in another aspect, a serial combination of the flatsection 174, undulation section 176, and another flat section 174 may berepeated as a group without departing from the scope of the presentteachings.

In one embodiment, the undulation layers 176 may be arranged relative toeach other such that the channels 182 defined by one layer extend alonga direction that is different than a direction of the channels 182 ofthe other layer. Such angled configurations (sometimes referred to as a“cross” configuration) of the channels will be described in greaterdetail herein below in context of other possible channel contours,configurations, and shapes.

FIG. 3C illustrates still another embodiment 190 of the heat exchangeelements 140 comprising a notched layer 192 disposed on a flat layer194. As illustrated in FIG. 3C, the sectional shape of the notched layer192 comprises a series of notches 196 spaced at selected distancesapart. In addition, the notched layer 192 and the flat layer 194 definea plurality of channels 200 through which air can flow. It should beappreciated by those skilled in the art that the configuration of theheat exchange elements 140, as illustrated in FIG. 3C, may also bereferred to as a notched flat (NF) configuration without departing fromthe scope of the present teachings.

It should also be appreciated by those skilled in the art that thevarious embodiments of the heat exchange elements 140 as previouslydescribed herein above comprise air flow channels that are generallyaligned along a single direction. Therefore, it should also beappreciated that any number of different sectional shapes, contours, orconfigurations of the elements 140 may be used to achieve such an airflow and, in addition, may be implemented without departing from thescope of the present teachings. Moreover, the sectional shape of a givenelement 140 may depend on various factors, such as manufacturingtechniques, structural requirements, air flow characteristics, heatexchange characteristics, etc.

In other embodiments, the channels 142, 182 formed via the heat exchangeelements 140 can be adapted to extend along various directions. Forexample, FIG. 3D illustrates one embodiment of the elements 140comprising at least two notched layers 210 combined in a manner suchthat the channels of one layer extend at an angle with respect tochannels of another layer. It should be appreciated by those skilled inthe art that this configuration may be referred to as a notched crossed(NC) configuration. In one aspect, this angled channel directionrelationship between the two layers is depicted in a plan view 214 as aplurality of solid lines 216 representing the notches 212 of one layer,and a plurality of dashed lines 218 representing the notches 212 of theother layer. The angle between the channel directions 216 and 218 may beselected to provide a suitable performance in terms of, by way ofexample, structural requirement and air flow characteristics.

FIG. 3E illustrates one embodiment 220 of the heat exchange elements 140having crossed channels. As illustrated in FIG. 3E, the elements 140comprises a first corrugated layer 222 and a second corrugated layer224. In one embodiment, the first corrugated layer 222 comprises aplurality of corrugations 226 that are larger than corrugations 230defined by a second corrugated layer 224. The larger corrugations 226define channels 232, and the smaller corrugations 230 define channels234. The relative directions of the corrugations 226 and 230 aredepicted in a plan view, wherein the larger corrugations 226 arerepresented as solid lines, and the smaller corrugations 230 arerepresented as dashed lines. When such two layers of corrugations areoriented in an angled manner, the channels 232 and 234 are crosscoupled, which may be advantageous in certain applications. In general,it should be apparent that any number of channel shapes and sizes may beutilized in the elements 140. Moreover, relative channel directionsbetween the adjacent layers may be selected in any number of wayswithout departing from the scope of the present teachings.

The various layers of the elements 140 described above may be formed inany number of ways known in the art. In one embodiment, the elements 140may be formed out of metal such as low carbon steel or stainless steel.It should be appreciated by those skilled in the art that other forms ofmetals, as well as any other material, may be used to form the elements140, wherein the material can be adapted to allow powder coatingthereon. For the metal based elements, the layers may be formed out ofsheet metal having various depending on the application orimplementation. It should be appreciated by those skilled in the artthat the sheet metal may comprise various thicknesses including but notlimited to 18, 22, or 24 gauge sheet metal without departing from thescope of the present teachings.

FIGS. 4A-4B illustrate a powder coating layer formed on a base material.In one embodiment, as illustrated in FIG. 4A, the base materialcomprises a base layer 242, such as any of the layers described herein.The base layer 242 defines a first surface 244 and a second surface 246,on which respective first and second powder coating layers 250, 252 areformed. Additionally, the first powder coating layer 250 has a firstthickness 254, and the second powder coating layer 252 has a secondthickness 256. It should be appreciated that, in various embodiments,the first and second thicknesses 254, 256 as well as the composition ofthe first and second powder coating layers 250, 252 may be similar.

FIG. 4B illustrates a base material 262 that does not have a layer-likestructure. In one embodiment, parts of the elements 140 may havenon-layer structural characteristics. In addition, a surface 264 definedby such base material 262 may also be powder coated so as to form apowder coating layer 270 having a thickness 272. In various embodiments,the powder coating layer 250, 252, 270 may be formed from powder coatingparticles so as to advantageously provide an operating temperature toapproximately 975° F. Aside from the high operating temperaturecapability, the powder coating layer provides mechanical durability aswell as improved chemical resistance to sulfur based compounds. In oneaspect, the coating thickness is in the range of approximately 0.0015″to approximately 0.0025″.

It should be appreciated by those skilled in the art that any number ofpowder coating materials may be used to form the powder coating layersfor the elements without departing from the scope of the presentteachings. Additionally, it should be appreciated that the type ofpowder coating particles and the thickness of the layer may varydepending on factors such as intended application and operatingconditions of the heat exchanger 100.

FIG. 5 illustrates one embodiment of an overall process 280 forfabricating a heat exchanger having power coated elements 140. Theprocess 280 begins at start state 282, and in a state 284 that follows,the heat exchanger elements 140 are prepared for assembly. Suchpreparation may include manufacturing or acquiring the elements orcomponents of the elements 140. In state 286 that follows, the elements140 or the components of the elements 140 are powder coated. The powdercoating step will be described in greater detail herein below.Following, in a state 288, the elements 140 are assembled. The process280 terminates in an end state 290.

FIG. 6 illustrates one embodiment of a process 300 for powder coatingthe heat exchange elements 140. It should be appreciated by thoseskilled in the art that such a process may occur in state 286 of theheat exchanger fabricating process 280 described above in reference toFIG. 5. In one aspect, the powder coating process 300 is performed onthe components of the elements 140. Advantageously, powder coating maybe applied to the separate layers of the elements 140 so as to improvethe uniformity of powder application.

In one embodiment, the process 300 begins at start state 302, and instate 304 that follows, the surface of the element is prepared forpowder coating. Such preparation may include cleaning and otherpre-powder application processes that are generally known in the art.Proceeding to state 306 that follows, the prepared elements 140 areelectrically connected to a selected electrical potential. In variousimplementations, such connection comprises electrical grounding of theelements 140. Next, in state 308, electrically charged coating particlesare sprayed onto the elements 140. In one aspect, the elements 140 maybe held at the selected electrical potential, which attracts the chargedcoating particles to the surface of the elements 140 and promotesadhesion thereto. Following, in state 310, the elements 140 with theapplied coating particles are cured so as to cause the coating particlesto substantially fuse with the surface of the elements 140 to therebyform a durable and resilient coating on the elements 140. Next, theprocess 300 terminates in an end state 312.

Advantageously, the Dupont based coating material, as previouslydescribed above with reference to FIGS. 4A-4B, may be used to achievethe approximate 975° F. operational temperature limit. In thisembodiment, the curing process in state 310 comprises baking the coatedcomponents of the elements 140 for approximately one hour at atemperature of approximately 1200° F. It should be appreciated by thoseskilled in the art that the use of different coating materials maydictate different curing procedures.

In one embodiment, the heat exchange elements 140 and the heatexchangers 100 fabricated in the foregoing manner provides variousadvantages over conventional types of coatings. Traditionally, the heatexchange elements 140 are typically dipped in an enamel material to forman enamel coating. Unfortunately, this type of coating is susceptible toair pockets being trapped within the coating layer, which can adverselyaffect the durability and reliability of the coating layer.Additionally, the enamel coating is likely more susceptible to crackingwhen subjected to mechanical stresses. These mechanical stresses mayarise, for example, during assembly of the heat exchanger when theelements are pressed together to form the segment, such as segment 130in FIG. 2, which can also be referred to as a “basket”. Moreover,additional mechanical stresses may be induced by thermal fluctuationsand/or vibrations associated with the operation of the heat exchanger.Unfortunately, cracks and other breaches of the enamel coating exposesthe underlying base layer to potentially corrosive materials. Forexample, if the heat exchanger is cleaned by a spray of water, the watercan work its way into the metal and promote corrosion. The corrosiveeffects may be exacerbated if the air contains corrosive particulates,such as sulfur based compounds.

Advantageously, the powder coating of the heat exchange elements 140 ofthe present teachings as described herein above provide improvedmechanical durability, resiliency, and performance to thereby provideimproved corrosion resistance. FIG. 7 illustrates one possibleapplication of the heat exchanger 100 having powder coated elements 140in a harsh operating condition. For example, fossil fuel burning powergenerators typically comprise a boiler 320 that burns the fossil fuel togenerate heat. As illustrated in FIG. 7, arrows 330 indicate the flow ofa flue gas that results from the burning and is eventually ejected intothe atmosphere. In some generators, the flue gas from the boiler 320 maypass through a selective catalytic reduction (SCR) reactor 322 to removea substantial portion of No_(x) present. The flue gas, whether from theboiler 320 or from the SCR reactor 322, then typically passes through aheat exchanger 324 to lower the gas temperature prior to being processedin an exhaust processor 326. It should be appreciated that the exhaustprocessor 326 may comprise an electrostatic precipitator that collectsparticulates from the gas and a smoke stack that ejects the gas to theenvironment.

As further illustrated in FIG. 7, the gas passing through the heatexchanger 324 may comprise a relatively high temperature and arelatively high concentration of particulates including sulfur basedcompounds. Therefore, the particulates may likely accumulate on the heatexchange elements 140, which may likely require routine cleanings.Because the powder coating on the elements 140 provides improvedmechanical durability, resiliency, and performance in a manner describedabove, the corrosive effects are mitigated in an improved manner.Advantageously, the powder coating of the heat exchange elements 140 maywithstand high operating temperatures with selected coating materials,such as the previously described Dupont based powder coating having arelatively large operational temperature limit. Therefore, the heatexchanger 100 having the powder coated heat exchange elements 140 of thepresent teachings are advantageously suited for high temperature andhigh sulfur environment applications, such as the fossil burninggenerators.

In some embodiments, powders used for coating preferably result in thecoating having properties that are desirable for heat exchangerapplications. These desirable properties include resiliency of theformed coating, high acid resistivity, and robust adherence to theunderlying metal surface. Additionally, the powders preferably inhibitthe adherence of sulfur-based particles to the powder coated surface anddecrease the accumulation of particles on the surface of the elements140. Powders that result in such properties in the heat exchangerapplications can include commercially available products such as thosefrom Cardinal Industrial Finishes of City of Industry, California.

One such powder comprises an E305-GR533 epoxy powder coatingformulation. The E305 has a specific gravity of approximately 1.56, withan average particle size of approximately 25-50 microns. The E305 powdercoat can be cured by heating at approximately 400 degrees F. forapproximately 10 minutes.

An exemplary E305 coat of approximately 2.0 to 4.5 mils thickness has adirect impact value of approximately 60 in-lbs using an industry D2794method, and an indirect impact value of approximately 60 in-lbs usingthe same method. The exemplary coating has a pencil hardness in the “2H”category using the industry D3363 method.

The E305 has been designed to be applied by electrostatic spray onmetals such as steel, galvanized steel, or aluminum, and the resultingcoat has a good to excellent chemical resistance to most solvents, oils,acids, and alkalies. Advantageously, the E305 powder can be reclaimed,sieved, and recycled.

Another powder available from Cardinal comprises a P004-GR16 polyesterpolyurethane powder coating formulation. The intended application,recyclability, chemical resistance property, and pencil hardness aresimilar to that of the E305 formulation. The P004 powder coat (of anexemplary coating thickness of approximately 1.5 to 3.0 mils) has directand indirect impact values of approximately 120 in-lbs. Such a coatingcan be achieved by heating the powder coat for approximately 12 minutesat approximately 400 degrees F.

Another powder available from Cardinal comprises a H305-GR10 epoxypolyester hybrid powder coating formulation. The intended application,recyclability, chemical resistance property, impact values and pencilhardness are similar to that of the P004 formulation. In addition to thechemical resistance property, the H305 coating provides an excellentresistance against salt spray and humidity. Using the industry ASTM B117method, the H305 coating exhibits approximately 1,000 hours of saltspray with less than approximately ⅛ inch creep from a scribe. Using theindustry ASTM D2247 method, the H305 coating exhibits approximately1,000 hours of humidity exposure with substantially no loss of adhesionor blistering. Such a coating can be achieved by heating the powder coatfor approximately 10 minutes at approximately 400 degrees F.

FIG. 8 illustrates another embodiment of a process 500 for powdercoating components of the heat exchanger 100. In one embodiment, thepowder coating is applied to the heat exchange elements 140. In anotherembodiment, the powder coating is applied to seals (radial 64 or axial70) between the radial walls 107 and the housing 104 (See FIG. 1). Suchseals are described in U.S. Pat. Nos. 5,950,707 and 5,881,799, theentire contents of which are incorporated by reference and should beconsidered a part of this specification.

FIG. 9 illustrates one embodiment of a seal assembly 72, which can beused with the heat exchanger 100. In one embodiment, the seal assembly72 can be the radial seal 70, wherein the seal assembly 72 is mounted onan outer surface of the radial wall 107 and provides a secure sealbetween the radial wall 107 and an inner surface of the housing 104. Inthis embodiment, the seal assembly 72 preferably inhibits leakage orbypass flow between the cold air conduit and the hot gas conduit throughthe area between the outer surface of the radial wall 107 and the innersurface of the housing 104. In another embodiment, the seal assembly 72can be the axial seal 64, wherein the seal assembly 72 is mounted on theouter radial edge of the radial wall 107 and provides a secure sealbetween the top or bottom edge of the radial wall 107 and an innersurface of the sector plates 110 a, 110 b of the housing 104. In thisembodiment, the seal assembly 72 preferably inhibits leakage or bypassflow between the cold air conduit and the hot gas conduit through thearea between the top or bottom edge of the radial wall 107 and an innersurface of the sector plate 110 a, 110 b of the housing 104

The seal assembly 72 includes an elongate and generally flat mountingstrip 74. Preferably, the mounting strip 74 extends along the entirelength of the seal assembly 72 and has a front surface 74 a and a rearsurface 74 b. A series of elongated apertures 80 extend through themounting strip 74 and are distributed along the length of the mountingstrip 80.

The seal assembly 72 also includes a resilient section 82. In oneembodiment, the resilient section 82 is bellows-shaped. In theillustrated embodiment, the resilient section 82 has a series ofcorrugations 83 that extend in and out of a plane defined by themounting strip 74 and are configured to compress and allow the resilientsection 82 to act as a spring. The resilient section 82 has a frontsurface 82 a and a rear surface 82 b.

The seal assembly 72 also includes a sealing strip 84 that extendsoutward from the resilient section 82 opposite the mounting strip 74.The sealing strip 84 preferably extends in a direction substantiallyparallel to a plane defined by the mounting strip 74 and has a frontsurface 84 a and a rear surface 84 b. The sealing strip 84 also has asubstantially straight outer edge 86. In one embodiment, where the sealassembly 72 is the radial seal 70, the sealing strip 84 preferably sealsthe juncture between the radial wall 107 and an inner surface of thehousing 104. In another embodiment, where the seal assembly 72 is theaxial seal 64, the sealing strip 84 preferably seals the juncturebetween the top or bottom edge of the radial wall 107 and an innersurface of one of the sector plates 110 a, 110 b of the housing 104.

FIG. 10 shows a side view of the seal assembly 72 used as the axial seal64. In the illustrated embodiment, the sealing assembly 72 is mounted tothe top edge of the radial wall 107 via at least one bolt 90 extendingthrough the apertures 80 in the mounting strip 74 and through the radialwall 107. A nut 92 is screwed onto the bolt 90 to secure the mountingstrip 74 to the radial wall 107. However, one of ordinary skill in theart will recognize that other mechanisms can be used to secure themounting strip 74 to the radial wall 107, such as welds and adhesives.

As shown in FIG. 10, various surfaces of the seal assembly 72 areexposed to the environment, which as discussed above, can inducecorrosion of the metal in the seal 72. As seen in FIG. 10, the rearsurface 74 b of the mounting strip 74 is disposed adjacent the radialwall 107, reducing the exposure of the rear surface 74 b to theenvironment. However, the front and rear surfaces 82 a, 82 b of theresilient section, and the front and rear surfaces 84 a, 84 b of thesealing strip would be exposed to the potentially corrosive environment.Similarly, when used as the radial seal 70, the exposure of the rearsurface 74 b of the mounting strip 74 would be reduced, while the restof the surfaces 82 a, 82 b, 84 a, 84 b would be exposed to thepotentially corrosive environment.

FIGS. 11A-13 illustrates another embodiment of a seal assembly. In theillustrated embodiment, the seal assembly is a perimeter orcircumferential seal assembly 430. In one configuration, shown on FIG.11A, the seal assembly 430 is fixedly attached to the rotor 102. Theseal assembly 430 can be attached to the rotor 102 in any suitablemanner. For example, in one embodiment the seal assembly 430 can bewelded to the rotor 102. In other embodiments, the seal assembly 430 canbe bolted to the rotor 102 or fixedly attached to the rotor 102 via aclamp. The seal 430 includes a mounting section 432 and a sealingsection 434. In the illustrated embodiment, the mounting section 432 isattached to an outer wall 422 of the rotor 102 and a mounting plate 436.The seal 430 is preferably bent so that the sealing section 434 ispositioned substantially adjacent a sealing surface 442 a which, in theillustrated embodiment, comprises an inner wall 424 of the housing 104.The mounting section 432 has a front surface 432 a and a rear surface432 b. In the illustrated embodiment, the front surface 432 a isadjacent the outer wall 422 and the rear surface 432 b is adjacent themounting plate 436. Likewise, the sealing section 434 has a frontsurface 434 a and a rear surface 434 b. In the illustrated embodiment,the front surface 434 a faces toward the inner wall 422 and the rearsurface 434 b faces toward the rotor 102. Preferably, the seal 430extends substantially across a bypass gap 420 so as to inhibit theability of intake air or exhaust gas to bypass the rotor 102.

As discussed above, various surfaces of the seal assembly 430 areexposed to the harsh environment proximal the heat exchanger 100, whichcan induce corrosion of the metal in the seal 430. As seen in FIG. 11A,the front and rear surface 432 a, 432 b of the mounting strip 432 aredisposed adjacent the outer wall 422 of the rotor 102 and mounting plate436, respectively. Therefore, the exposure of the surfaces 432 a, 432 bof the mounting section 432 to the corrosive environment may be reduced.However, the rear surface 434 b of the sealing section 434 faces therotor 102 and is exposed to the harsh corrosive environment. The frontsurface 434 a of the sealing section 434 faces away from the rotor 102,which may reduce the exposure of the front surface 434 a to thecorrosive environment due to the sealing effect of the sealing section434 against the inner surface 424 of the housing 104.

FIG. 11B illustrates another configuration of the perimeter seal 430mounted in the bypass gap 420 to inhibit intake air or exhaust gas frombypassing the rotor 102. In the illustrated embodiment, the mountingsection 432 is bolted to the inner wall 424 of the housing 104,preferably adjacent the upper and lower ends of the housing 104. Howeverother mechanisms can be used to attach the mounting section 432 to theinner wall 424, such as welds. In the illustrated embodiment, thesealing section 434 extends into the bypass gap 420 so as to bepositioned adjacent a sealing surface 442 b. In the illustratedembodiment, the sealing surface 442 b is a sealing plate 456 thatextends circumferentially around the rotor 102. In the illustratedembodiment, the front surface 432 a of the mounting section 432 facesgenerally toward the rotor 102, while the rear surface 432 b is adjacentthe inner wall 424. Similarly, the front surface 434 a of the sealingsection 434 faces generally toward the rotor 102, while the rear surface434 b faces generally toward the inner wall 424.

As seen in FIG. 11B, the rear surface 432 b of the mounting strip 432 isdisposed adjacent the inner wall 424 of the housing 104. Therefore, theexposure of the rear surface 432 b of the mounting section 432 to thecorrosive environment may be reduced. However, the front surface 432 aof the mounting section 432 faces the rotor 102 and is exposed to theharsh corrosive environment. Likewise, the front surface 434 a of thesealing section 434 faces the rotor 102 and is exposed to the corrosiveenvironment. The rear surface 434 a of the sealing section 434 facesaway from the rotor 102, which may reduce the exposure of the frontsurface 434 a to the corrosive environment due to the sealing effect ofthe sealing section 434 against the sealing plate 256.

FIGS. 12 and 13 illustrate further details of the perimeter seal 430.The seal 430 comprises a first seal member 430 a and a second sealmember 430 b, both of which include mounting sections 432 and sealingsections 434. The first and second seal members 430 a, 430 b each have aseries of alternating tabs 435 a, 435 b, 435 c and slots that definerecesses 447, wherein the tabs 435 a of the first seal member 430 areconfigured to fit through the slots 437 b of the second seal member 430b to engage the tabs 435 b of the second seal member 430 b, and viceversa.

In particular, alternating neck sections 443 of the tabs 435 arepositioned in the rectangular recesses 437. The neck sections 443 of thetabs 435 preferably do not significantly overlap, however, the sealingupper sections 442 of the tabs 435 do overlap. Each tab 435 ispreferably positioned in the slots so that a first lateral side 460 a ofa tab 435 a on the first member 430 a is positioned adjacent a firstface 452 of a first tab 435 b on the second member 430 b. The tab 435 aon the first member 430 a then has a bent section 454 so that a secondlateral side 460 b of the tab 435 a is positioned adjacent a second face454, opposite the first face 452, of the second tab 235 c on the secondmember 430 b. Further details of the perimeter seal 430 are provided inU.S. Pat. No. 5,881,799.

With continued reference to FIG. 8, the process 500 includes the step510 of preparing the surface of the component to be coated. In oneembodiment, where the component is a seal, the seal can be made of AISI4130 normalized steel. However, one of ordinary skill in the art willrecognize that other suitable materials can be used. In the present step510, a line grain is preferably produced on the surface of thecomponent. Said line grain preferably provides a textured finish with aporous effect to facilitate the application of the powder coating to thecomponent surface. In one preferred embodiment, the line grain is formedon the surface in a generally linear direction to provide a brushedfinish. In another embodiment, the line grain can be formed on thesurface of the component in a generally non-linear direction. Preferablya 60 grit Iron Oxide Belt is used to form said line grain. However, anysuitable mechanism can also be used to form the line grain. In oneembodiment, where the component being coated is a large seal, thesurface is preferably sandblasted following the line grain formationprocess. Preferably, the surface is sandblasted with an even texture 80grit aluminum oxide media. However, any other suitable media can beused.

Following the surface preparation step 510, the component surface ispreferably cleaned, as illustrated in Step 520. In one embodiment, anIron phosphate wash is applied to the component surface to clean thesurface. Preferably, the wash substantially removes oil and wastematerial generated in the surface preparation step 510 from thecomponent surface. In a preferred embodiment, the wash is applied so asto provide a coating of between about 300 mg/m² and about 900 mg/m². Ina preferred embodiment, step 520 also includes application of a rinse ofthe component surface. In one embodiment, the component surface isrinsed with de-ionized water. In another embodiment, the componentsurface is rinsed with regular water. The component is then heated(i.e., baked) to remove moisture from the component surface. In oneembodiment, the component is baked at a temperature of between about 50deg. F and about 500 deg. F for a period of between about five minutesand about two hours. In another embodiment, the component is baked at atemperature of about 400 deg. F for a period of about 20 minutes.However, other suitable mechanisms known in the art can be used toremove moisture from the component surface.

The process 500 also includes the step 530 of applying the powdercoating to the component surface. Preferably, the powder coating issprayed onto the component surface. In one embodiment, the powdercoating is epoxy resin model Resicoat R4-ES HJF14R (500547) from AkzoNobel of The Netherlands. However, other suitable powder coatingmaterials can be used that have similar corrosion resistance, chemicalresistance, heat resistance, impact resistance, flexibility and adhesioncharacteristics. Preferably, the powder coating is applied using the ISO8130-2 procedure and preferably results in a coating thickness of about3-5 mils. In another embodiment, the procedure results in a coating areadensity of between about 1.55 and about 175 grams per cm².

Following the application of the powder coating to the component surface(Step 530), the component surface is preferably cured (Step 540). In oneembodiment, the component is preheated to a desired temperature. In oneembodiment, the component surface is preheated to a temperature ofbetween about 50 deg. F and about 600 deg. F for a period of betweenabout 3 minutes and about 2 hours. In another embodiment, the componentsurface is preheated to a temperature of about 320 deg. F for a periodof about 5 minutes. The component surface is then cured. In onepreferred embodiment, the component surface is cured at a temperature ofbetween about 50 deg. F. and about 1000 deg. F for a period of betweenabout five minutes and about two hours. In another embodiment, thecomponent surface is cured at a temperature of about 400 deg. F for aperiod of about 20 to 30 minutes. Preferably, the powder coatingachieves a hardness in the range of between about HB and 5H during thecuring process using, for example, an ASTM Method D3363 pencil hardnessstandard. One of ordinary skill in the art will recognize that theapplication (Step 530) and curing (Step 540) of the component surfacecan in some embodiments be performed intermittently.

Following the curing of the powder coating (Step 540), the component canoptionally be inspected (Step 550). In a preferred embodiment, componentis inspected to ensure that the coverage and the surface texture flow ofthe powder coating is within a desired range. For example, the componentsurface can be inspected to ensure the surface texture flow meets adesired smoothness.

In one embodiment, the heat exchanger 100 is assembled following thepowder coating of the components. For example, where the components areseals, the powder coated seals 64, 70 can be attached to the walls 107and the heat exchange rotor 102 mounted within the housing 104.

Although the above-disclosed embodiments of the present teachings haveshown, described, and pointed out the fundamental novel features of theinvention as applied to the above-disclosed embodiments, it should beunderstood that various omissions, substitutions, and changes in theform of the detail of the devices, systems, and/or methods illustratedmay be made by those skilled in the art without departing from the scopeof the present teachings. Consequently, the scope of the inventionshould not be limited to the foregoing description, but should bedefined by the appended claims.

What is claimed is:
 1. A component for use in a regenerative heatexchanger having a heat exchanging body and a housing, the componentattachable to the heat exchanging body, the component comprising: one ormore elements configured to facilitate heat exchange with a gas thatflows through the heat exchanging body during operation of the heatexchanger, wherein the one or more elements include a protective coatingdisposed on an underlying surface thereof, the protective coatingcomprising a resilient powder coating having a coating thicknessconfigured to inhibit cracking during flexion of the elements andfurther configured to inhibit corrosion inducing agents from contactingthe underlying surface of the one or more elements to inhibit corrosionof the elements while not inhibiting heat transfer between the elementsand said airflow.
 2. The component of claim 1, wherein the protectivecoating has a contact area density of between about 1.55 g/cm² and about6 g/cm².
 3. The component of claim 2, wherein the contact area densityis between about 1.55 g/cm² and about 2.5 g/cm².
 4. The component ofclaim 1, wherein the thickness of the powder coating on said underlyingsurface is between about 1.5 mils and about 2.5 mils, said thicknessconfigured to inhibit said corrosion inducing agents from contactingsaid underlying surface of the elements to thereby resist corrosion ofthe one or more elements.
 5. The component of claim 1, wherein thethickness of the powder coating on said underlying surface is betweenabout 2 mils and about 4 mils, said thickness configured to inhibit saidcorrosion inducing agents from contacting said underlying surface of theelements to thereby resist corrosion of the one or more elements
 6. Thecomponent of claim 1, wherein the powder coating has an operationaltemperature limit of up to approximately 975° F.
 7. The component ofclaim 1, wherein the one or more elements comprise a plurality of heatexchange elements in a heat exchange basket.
 8. The component of claim1, wherein the coating has a hardness of between about HB and about 5Hper an ASTM Method D3363 pencil hardness standard.
 9. The component ofclaim 1, wherein the powder coating has a direct and indirect impactvalue of between 60 in-lbs and 120 in-lbs using an ASTM Method D2794impact standard.
 10. The component of claim 1, wherein the one or moreelements comprise one or more radial or circumferential seals coupleableto the heat exchanging body.
 11. A component for use in a regenerativeheat exchanger having a heat exchanging body and a housing, thecomponent attachable to the heat exchanging body, the componentcomprising: one or more elements configured to facilitate heat exchangewith a fluid that flows through the heat exchanging body duringoperation of the heat exchanger, wherein the one or more elementsinclude a protective coating disposed on a surface thereof, theprotective coating comprising a resilient powder coating configured towithstand a temperature of up to approximately 1000° F., the powdercoating configured to inhibit cracking during flexion of the elementsand further configured to inhibit corrosion inducing agents fromcontacting an underlying surface of the one or more elements to inhibitcorrosion of the elements while not inhibiting heat transfer between theelements and said airflow.
 12. The component of claim 11, wherein theprotective coating has a coating area density on said underlying surfaceis between about 1.55 g/cm² and about 175 g/cm².
 13. The component ofclaim 12, wherein the protective coating has a coating area density onsaid underlying surface is between about 1.55 g/cm² and about 6 g/cm².14. The component of claim 13, wherein the coating area density on saidunderlying surface is between about 1.55 g/cm² and about 2.5 g/cm². 15.The component of claim 11, wherein the thickness of the powder coatingon said surface is between about 1.5 mils and about 2.5 mils, saidthickness configured to inhibit said corrosion inducing agents fromcontacting said underlying surface of the elements to thereby resistcorrosion of the one or more elements.
 16. The component of claim 11,wherein the one or more elements comprise a plurality of heat exchangeelements in a heat exchange basket.
 17. The component of claim 11,wherein the powder coating has a hardness of between about HB and about5H per an ASTM Method D3363 pencil hardness standard.
 18. The componentof claim 11, wherein the powder coating has a direct and indirect impactvalue of between 60 in-lbs and 120 in-lbs using an ASTM Method D2794impact standard.
 19. The component of claim 11, wherein the one or moreelements comprise one or more radial or circumferential seals coupleableto the heat exchanging body.